Optimal guidance for hypersonic vehicle using analytical solutions and an intelligent reversal strategy

Author:

Zhou Hongyu,Li XunORCID,Bai Yuliang,Wang Xiaogang

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference46 articles.

1. Fixed-time actuator fault accommodation applied to hypersonic gliding vehicles;Yu;IEEE Trans. Autom. Sci. Eng.,2021

2. A predictor-corrector time integration algorithm for dynamic analysis of nonlinear systems;Lopez;Nonlinear Dyn.,2020

3. A novel reentry trajectory generation method using improved particle swarm optimization;Zhou;IEEE Trans. Veh. Technol.,2020

4. Entry guidance with terminal time control based on quasi- equilibrium glide condition;Guo;IEEE Trans. Aerosp. Electron. Syst.,2020

5. Quasi-continuous high-order sliding mode controller design for reusable launch vehicles in reentry phase;Tian;Aerosp. Sci. Technol.,2013

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